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SE9802707L - Burner chamber device and method for reducing the influence of acoustic pressure fluctuations in a burner chamber device - Google Patents

Burner chamber device and method for reducing the influence of acoustic pressure fluctuations in a burner chamber device

Info

Publication number
SE9802707L
SE9802707L SE9802707A SE9802707A SE9802707L SE 9802707 L SE9802707 L SE 9802707L SE 9802707 A SE9802707 A SE 9802707A SE 9802707 A SE9802707 A SE 9802707A SE 9802707 L SE9802707 L SE 9802707L
Authority
SE
Sweden
Prior art keywords
chamber device
combustion chamber
burner
burner chamber
influence
Prior art date
Application number
SE9802707A
Other languages
Swedish (sv)
Other versions
SE9802707D0 (en
Inventor
Leif G Andersson
Original Assignee
Abb Ab
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Abb Ab filed Critical Abb Ab
Priority to SE9802707A priority Critical patent/SE9802707L/en
Publication of SE9802707D0 publication Critical patent/SE9802707D0/en
Priority to PCT/SE1999/001308 priority patent/WO2000009945A1/en
Priority to US09/762,639 priority patent/US6430930B1/en
Priority to JP2000565348A priority patent/JP4511044B2/en
Priority to AU56608/99A priority patent/AU5660899A/en
Priority to DE69917655T priority patent/DE69917655T2/en
Priority to RU2001106647/06A priority patent/RU2222751C2/en
Priority to EP99943533A priority patent/EP1108184B1/en
Priority to CA002340391A priority patent/CA2340391C/en
Publication of SE9802707L publication Critical patent/SE9802707L/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D23/00—Assemblies of two or more burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M20/00—Details of combustion chambers, not otherwise provided for, e.g. means for storing heat from flames
    • F23M20/005—Noise absorbing means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/96—Preventing, counteracting or reducing vibration or noise
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2210/00—Noise abatement
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Spray-Type Burners (AREA)

Abstract

The invention refers to a combustion chamber device including a combustion chamber (2) and a set of burners (6) with an outlet opening (7) in the combustion chamber. Each burner includes members (10) for the supply of a flow of oxygen-containing gas, members (8) for the supply of fuel, and a space (9), which extends to the combustion chamber (2) for mixing of the fuel and the oxygen-containing gas. Each burner (6) is arranged to convey a substantially equally large flow of oxygen-containing gas through the burner to the combustion chamber. Each burner (6) is defined by at least one parameter including a characteristic length (a) of the space (9) along the longitudinal direction (x). At least the characteristic length (a) of at least one of the burners is selected in such a way that it deviates from the corresponding length (a) of another burner and in such a way that the influence of the oscillations which arise during operation of the combustion chamber device are reduced.
SE9802707A 1998-08-11 1998-08-11 Burner chamber device and method for reducing the influence of acoustic pressure fluctuations in a burner chamber device SE9802707L (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
SE9802707A SE9802707L (en) 1998-08-11 1998-08-11 Burner chamber device and method for reducing the influence of acoustic pressure fluctuations in a burner chamber device
PCT/SE1999/001308 WO2000009945A1 (en) 1998-08-11 1999-07-23 Arrangement for reduction of acoustinc vibrations in a combustion chamber
US09/762,639 US6430930B1 (en) 1998-08-11 1999-07-23 Arrangement for reduction of acoustic vibrations in a combustion chamber
JP2000565348A JP4511044B2 (en) 1998-08-11 1999-07-23 Configuration to reduce acoustic vibration in the combustion chamber
AU56608/99A AU5660899A (en) 1998-08-11 1999-07-23 Arrangement for reduction of acoustinc vibrations in a combustion chamber
DE69917655T DE69917655T2 (en) 1998-08-11 1999-07-23 SYSTEM FOR CONTROLLING ACOUSTIC VIBRATIONS IN A COMBUSTION CHAMBER
RU2001106647/06A RU2222751C2 (en) 1998-08-11 1999-07-23 Arrangement for reducing acoustic vibrations in combustion chamber
EP99943533A EP1108184B1 (en) 1998-08-11 1999-07-23 Arrangement for reduction of acoustic vibrations in a combustion chamber
CA002340391A CA2340391C (en) 1998-08-11 1999-07-23 Arrangement for reduction of acoustic vibrations in a combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE9802707A SE9802707L (en) 1998-08-11 1998-08-11 Burner chamber device and method for reducing the influence of acoustic pressure fluctuations in a burner chamber device

Publications (2)

Publication Number Publication Date
SE9802707D0 SE9802707D0 (en) 1998-08-11
SE9802707L true SE9802707L (en) 2000-02-12

Family

ID=20412229

Family Applications (1)

Application Number Title Priority Date Filing Date
SE9802707A SE9802707L (en) 1998-08-11 1998-08-11 Burner chamber device and method for reducing the influence of acoustic pressure fluctuations in a burner chamber device

Country Status (9)

Country Link
US (1) US6430930B1 (en)
EP (1) EP1108184B1 (en)
JP (1) JP4511044B2 (en)
AU (1) AU5660899A (en)
CA (1) CA2340391C (en)
DE (1) DE69917655T2 (en)
RU (1) RU2222751C2 (en)
SE (1) SE9802707L (en)
WO (1) WO2000009945A1 (en)

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EP1255074B1 (en) * 2001-05-01 2005-11-23 Alstom Technology Ltd Oscillation reduction in a combustion chamber
JP2003065537A (en) * 2001-08-24 2003-03-05 Mitsubishi Heavy Ind Ltd Gas turbine combustor
US6931853B2 (en) * 2002-11-19 2005-08-23 Siemens Westinghouse Power Corporation Gas turbine combustor having staged burners with dissimilar mixing passage geometries
EP1493972A1 (en) * 2003-07-04 2005-01-05 Siemens Aktiengesellschaft Burner unit for a gas turbine and gas turbine
US20050026100A1 (en) * 2003-07-14 2005-02-03 Hawkins Samuel D. Inshot burner
WO2007113130A1 (en) * 2006-03-30 2007-10-11 Alstom Technology Ltd Burner arrangement, preferably in a combustion chamber for a gas turbine
US20090061369A1 (en) * 2007-08-28 2009-03-05 Gas Technology Institute Multi-response time burner system for controlling combustion driven pulsation
US8028512B2 (en) 2007-11-28 2011-10-04 Solar Turbines Inc. Active combustion control for a turbine engine
EP2119966A1 (en) * 2008-05-15 2009-11-18 ALSTOM Technology Ltd Combustor with reduced carbon monoxide emissions
EP2119964B1 (en) 2008-05-15 2018-10-31 Ansaldo Energia IP UK Limited Method for reducing emissons from a combustor
US7578130B1 (en) * 2008-05-20 2009-08-25 General Electric Company Methods and systems for combustion dynamics reduction
IT1391245B1 (en) * 2008-08-08 2011-12-01 Ansaldo Energia Spa METHOD FOR DETERMINING THE PLACEMENT OF BURNERS IN A ANULAR COMBUSTION CHAMBER OF A GAS TURBINE
DE102008053755A1 (en) 2008-10-28 2010-04-29 Pfeifer, Uwe, Dr. Arrangement for extension of stability range of pilot flame system and/or pilot burner system in e.g. aircraft, has burner systems with burners distributed radially at periphery of chamber or over cross-section area of chamber
US20100192578A1 (en) * 2009-01-30 2010-08-05 General Electric Company System and method for suppressing combustion instability in a turbomachine
US20110048022A1 (en) * 2009-08-29 2011-03-03 General Electric Company System and method for combustion dynamics control of gas turbine
US8322140B2 (en) * 2010-01-04 2012-12-04 General Electric Company Fuel system acoustic feature to mitigate combustion dynamics for multi-nozzle dry low NOx combustion system and method
FR2958014B1 (en) * 2010-03-23 2013-12-13 Snecma COMBUSTION CHAMBER WITH INJECTORS SHIFTING LONGITUDINALLY ON THE SAME CROWN
EP2423598A1 (en) 2010-08-25 2012-02-29 Alstom Technology Ltd Combustion Device
US8875516B2 (en) * 2011-02-04 2014-11-04 General Electric Company Turbine combustor configured for high-frequency dynamics mitigation and related method
CN103080653B (en) * 2011-03-16 2015-03-25 三菱日立电力系统株式会社 Gas turbine combustor and gas turbine
RU2561956C2 (en) * 2012-07-09 2015-09-10 Альстом Текнолоджи Лтд Gas-turbine combustion system
US8966909B2 (en) * 2012-08-21 2015-03-03 General Electric Company System for reducing combustion dynamics
US20140083111A1 (en) * 2012-09-25 2014-03-27 United Technologies Corporation Gas turbine asymmetric fuel nozzle combustor
US9546601B2 (en) * 2012-11-20 2017-01-17 General Electric Company Clocked combustor can array
WO2014086731A1 (en) 2012-12-05 2014-06-12 Deutsches Zentrum für Luft- und Raumfahrt e.V. Method for operating a combustion system and combustion system
US9650959B2 (en) * 2013-03-12 2017-05-16 General Electric Company Fuel-air mixing system with mixing chambers of various lengths for gas turbine system
JP6021705B2 (en) * 2013-03-22 2016-11-09 三菱重工業株式会社 Combustor and gas turbine
EP2796789B1 (en) * 2013-04-26 2017-03-01 General Electric Technology GmbH Can combustor for a can-annular combustor arrangement in a gas turbine
US20140345287A1 (en) * 2013-05-21 2014-11-27 General Electric Company Method and system for combustion control between multiple combustors of gas turbine engine
US9709279B2 (en) 2014-02-27 2017-07-18 General Electric Company System and method for control of combustion dynamics in combustion system
US9845956B2 (en) * 2014-04-09 2017-12-19 General Electric Company System and method for control of combustion dynamics in combustion system
US9845732B2 (en) * 2014-05-28 2017-12-19 General Electric Company Systems and methods for variation of injectors for coherence reduction in combustion system
US10775043B2 (en) * 2014-10-06 2020-09-15 Siemens Aktiengesellschaft Combustor and method for damping vibrational modes under high-frequency combustion dynamics
WO2016068922A1 (en) * 2014-10-30 2016-05-06 Siemens Aktiengesellschaft Pilot burner and method for stabilizing a pilot flame in a combustor subject to combustion dynamics
KR102063169B1 (en) * 2017-07-04 2020-01-07 두산중공업 주식회사 Fuel nozzle assembly and combustor and gas turbine having the same

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Also Published As

Publication number Publication date
CA2340391A1 (en) 2000-02-24
JP2002522741A (en) 2002-07-23
WO2000009945A1 (en) 2000-02-24
CA2340391C (en) 2008-09-23
RU2222751C2 (en) 2004-01-27
EP1108184B1 (en) 2004-05-26
AU5660899A (en) 2000-03-06
US6430930B1 (en) 2002-08-13
DE69917655D1 (en) 2004-07-01
JP4511044B2 (en) 2010-07-28
SE9802707D0 (en) 1998-08-11
EP1108184A1 (en) 2001-06-20
DE69917655T2 (en) 2005-06-16

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